FR2938923B1 - Procede et systeme de surveillance de parametres d'un aeronef. - Google Patents

Procede et systeme de surveillance de parametres d'un aeronef.

Info

Publication number
FR2938923B1
FR2938923B1 FR0806589A FR0806589A FR2938923B1 FR 2938923 B1 FR2938923 B1 FR 2938923B1 FR 0806589 A FR0806589 A FR 0806589A FR 0806589 A FR0806589 A FR 0806589A FR 2938923 B1 FR2938923 B1 FR 2938923B1
Authority
FR
France
Prior art keywords
aircraft
monitoring parameters
displayed
hand
ias
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
FR0806589A
Other languages
English (en)
Other versions
FR2938923A1 (fr
Inventor
Jean Damien Perrie
Guillaume Preaux
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Operations SAS
Original Assignee
Airbus Operations SAS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Airbus Operations SAS filed Critical Airbus Operations SAS
Priority to FR0806589A priority Critical patent/FR2938923B1/fr
Priority to US12/622,560 priority patent/US8352187B2/en
Publication of FR2938923A1 publication Critical patent/FR2938923A1/fr
Application granted granted Critical
Publication of FR2938923B1 publication Critical patent/FR2938923B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P1/00—Details of instruments
    • G01P1/07—Indicating devices, e.g. for remote indication
    • G01P1/08—Arrangements of scales, pointers, lamps or acoustic indicators, e.g. in automobile speedometers
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P5/00—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft
    • G01P5/14—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring differences of pressure in the fluid
    • G01P5/16—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring differences of pressure in the fluid using Pitot tubes, e.g. Machmeter
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P5/00—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft
    • G01P5/26—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring the direct influence of the streaming fluid on the properties of a detecting optical wave
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S17/00—Systems using the reflection or reradiation of electromagnetic waves other than radio waves, e.g. lidar systems
    • G01S17/02—Systems using the reflection of electromagnetic waves other than radio waves
    • G01S17/50—Systems of measurement based on relative movement of target
    • G01S17/58—Velocity or trajectory determination systems; Sense-of-movement determination systems

Abstract

Selon l'invention, le système de surveillance (1) comporte deux anémomètres laser (7A, 8A) et un dispositif logique de sélection (9) apte à sélectionner, d'une part, une valeur de la vitesse air IAS à afficher sur des premiers moyens d'affichage (5) et, d'autre part, une autre valeur de la vitesse air IAS à afficher sur des seconds moyens d'affichage (6).
FR0806589A 2008-11-24 2008-11-24 Procede et systeme de surveillance de parametres d'un aeronef. Active FR2938923B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR0806589A FR2938923B1 (fr) 2008-11-24 2008-11-24 Procede et systeme de surveillance de parametres d'un aeronef.
US12/622,560 US8352187B2 (en) 2008-11-24 2009-11-20 Method and system for monitoring parameters of an aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0806589A FR2938923B1 (fr) 2008-11-24 2008-11-24 Procede et systeme de surveillance de parametres d'un aeronef.

Publications (2)

Publication Number Publication Date
FR2938923A1 FR2938923A1 (fr) 2010-05-28
FR2938923B1 true FR2938923B1 (fr) 2011-02-11

Family

ID=40790888

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0806589A Active FR2938923B1 (fr) 2008-11-24 2008-11-24 Procede et systeme de surveillance de parametres d'un aeronef.

Country Status (2)

Country Link
US (1) US8352187B2 (fr)
FR (1) FR2938923B1 (fr)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9128109B1 (en) * 2012-08-20 2015-09-08 The Boeing Company Method and system for detecting errors in indicated air speed
FR2999293B1 (fr) * 2012-12-11 2015-01-16 Thales Sa Systeme pour la fourniture d'estimations de parametres de vol d'un aeronef independantes et dissimilaires et aeronef associe
US9146250B2 (en) 2013-07-23 2015-09-29 Gulfstream Aerospace Corporation Methods and systems for displaying backup airspeed of an aircraft
US20170276790A1 (en) * 2016-03-22 2017-09-28 Honeywell International Inc. Hybrid air data systems using lidar and legacy air data sensors
US10837813B2 (en) 2016-08-25 2020-11-17 The Trustees Of Princeton University Nanowires integration for real-time compensation
US11592838B2 (en) * 2018-02-28 2023-02-28 Instrumems Inc. Velocity sensing for aircraft

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2611040B1 (fr) * 1987-02-12 1989-06-30 Sfim Systeme autonome de mesure cinematique pour helicoptere
FR2613078B1 (fr) * 1987-03-26 1990-12-28 Crouzet Sa Dispositif de mesure de la vitesse air d'un helicoptere
FR2725033B1 (fr) * 1994-09-22 1997-01-03 Sextant Avionique Procede et systeme de determination des parametres anemobaroclinometriques a bord d'un aeronef
US6250149B1 (en) * 1999-04-08 2001-06-26 The Boeing Company System and method for generating aircraft flight data using a flush-mounted air data system
EP1525484B1 (fr) * 2002-08-02 2007-05-02 Ophir Corporation Systeme et procede optique de mesure de parametres de l'air
US6871487B2 (en) * 2003-02-14 2005-03-29 Kulite Semiconductor Products, Inc. System for detecting and compensating for aerodynamic instabilities in turbo-jet engines
FR2891368B1 (fr) 2005-09-27 2007-11-30 Airbus France Sas Systeme de surveillance de parametres anemobaroclinometriques pour aeronefs

Also Published As

Publication number Publication date
FR2938923A1 (fr) 2010-05-28
US8352187B2 (en) 2013-01-08
US20100131230A1 (en) 2010-05-27

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